Investigation of wing rock on delta wing part 1 : flow field and hydrodynamic force analysis

All modern fighter jets incorporate the use of the delta wing in the aircraft design to reduce wave drag and enhance flight performance at supersonic speeds. Delta wings are capable of providing increased lift compared to conventional airfoils due to the suction force generated by the leading edge v...

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Main Author: Gan, Calvin Cheng Rui
Other Authors: Sutthiphong Srigrarom
Format: Final Year Project
Language:English
Published: 2009
Subjects:
Online Access:http://hdl.handle.net/10356/16135
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Institution: Nanyang Technological University
Language: English
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spelling sg-ntu-dr.10356-161352023-03-04T18:16:14Z Investigation of wing rock on delta wing part 1 : flow field and hydrodynamic force analysis Gan, Calvin Cheng Rui Sutthiphong Srigrarom School of Mechanical and Aerospace Engineering DRNTU::Engineering::Aeronautical engineering::Aerodynamics All modern fighter jets incorporate the use of the delta wing in the aircraft design to reduce wave drag and enhance flight performance at supersonic speeds. Delta wings are capable of providing increased lift compared to conventional airfoils due to the suction force generated by the leading edge vortices. However, at high angles of attack, delta wings are also prone to a phenomenon known as wing rock which can occur at high angles of attack and subsonic speeds. This final year project focuses on the study of wing rock of delta wings at high angles of attack in a water tunnel. In the experiment, the hydrodynamic force generated by the delta wing is measured using a force-moment transducer, and the flow visualization is carried out with a dye probe, video camera and a digital SLR. Four delta wings, one Free To Roll device (FTR) and numerous angled joints were designed specifically for this experiment. Special attention was dedicated to the FTR device such that it only allowed movement around the longitudinal axis of the delta wing, and that special water-proof bearings were used to withstand the testing conditions. Experimental data suggests that the wing rock motion is dependent on asymmetrical vortex breakdown over the wing. Discrepancies with other studies could be due to different friction used between systems, which can have a significant on the propagation of wing rock. The conclusion from this study is that there is good correlation between angle of attack, delta wing sweep angle, Reynolds number and the vortex breakdown behavior. In addition, dye flow visualization results show that the asymmetric vortex breakdown occurs at certain conditions. Bachelor of Engineering (Aerospace Engineering) 2009-05-21T06:35:02Z 2009-05-21T06:35:02Z 2009 2009 Final Year Project (FYP) http://hdl.handle.net/10356/16135 en Nanyang Technological University 127 p. application/pdf
institution Nanyang Technological University
building NTU Library
continent Asia
country Singapore
Singapore
content_provider NTU Library
collection DR-NTU
language English
topic DRNTU::Engineering::Aeronautical engineering::Aerodynamics
spellingShingle DRNTU::Engineering::Aeronautical engineering::Aerodynamics
Gan, Calvin Cheng Rui
Investigation of wing rock on delta wing part 1 : flow field and hydrodynamic force analysis
description All modern fighter jets incorporate the use of the delta wing in the aircraft design to reduce wave drag and enhance flight performance at supersonic speeds. Delta wings are capable of providing increased lift compared to conventional airfoils due to the suction force generated by the leading edge vortices. However, at high angles of attack, delta wings are also prone to a phenomenon known as wing rock which can occur at high angles of attack and subsonic speeds. This final year project focuses on the study of wing rock of delta wings at high angles of attack in a water tunnel. In the experiment, the hydrodynamic force generated by the delta wing is measured using a force-moment transducer, and the flow visualization is carried out with a dye probe, video camera and a digital SLR. Four delta wings, one Free To Roll device (FTR) and numerous angled joints were designed specifically for this experiment. Special attention was dedicated to the FTR device such that it only allowed movement around the longitudinal axis of the delta wing, and that special water-proof bearings were used to withstand the testing conditions. Experimental data suggests that the wing rock motion is dependent on asymmetrical vortex breakdown over the wing. Discrepancies with other studies could be due to different friction used between systems, which can have a significant on the propagation of wing rock. The conclusion from this study is that there is good correlation between angle of attack, delta wing sweep angle, Reynolds number and the vortex breakdown behavior. In addition, dye flow visualization results show that the asymmetric vortex breakdown occurs at certain conditions.
author2 Sutthiphong Srigrarom
author_facet Sutthiphong Srigrarom
Gan, Calvin Cheng Rui
format Final Year Project
author Gan, Calvin Cheng Rui
author_sort Gan, Calvin Cheng Rui
title Investigation of wing rock on delta wing part 1 : flow field and hydrodynamic force analysis
title_short Investigation of wing rock on delta wing part 1 : flow field and hydrodynamic force analysis
title_full Investigation of wing rock on delta wing part 1 : flow field and hydrodynamic force analysis
title_fullStr Investigation of wing rock on delta wing part 1 : flow field and hydrodynamic force analysis
title_full_unstemmed Investigation of wing rock on delta wing part 1 : flow field and hydrodynamic force analysis
title_sort investigation of wing rock on delta wing part 1 : flow field and hydrodynamic force analysis
publishDate 2009
url http://hdl.handle.net/10356/16135
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